Trajectory analysis of transfers between L4 and L5 and low lunar orbit

Details Trajectory analysis of transfers between L4 and L5 and low lunar orbit Trajectory analysis of transfers between L4 and L5 and low lunar orbit

Oct 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988stin...8915144.&link_type=abstract

Unknown

Computer Science

Performance

Libration, Lunar Bases, Mission Planning, Spacecraft Performance, Spacecraft Trajectories, Transfer Orbits, Bouguer Law, Earth (Planet), Gravitational Effects, Many Body Problem, Moon

Scientific paper

The flight characteristics and spacecraft performance during missions
involving flight between the equilateral libration points and the Moon
are discussed. The conclusions drawn will show that a minimum energy
trajectory is the most efficient transfer technique for this type of
flight.

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